mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-08 02:17:07 +08:00
Moved filter states to stack RAM space
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@@ -72,38 +72,6 @@
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__EXPORT int attitude_estimator_ekf_main(int argc, char *argv[]);
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static unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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static float dt = 0.005f;
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/* state vector x has the following entries [ax,ay,az||mx,my,mz||wox,woy,woz||wx,wy,wz]' */
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static float z_k[9] = {0.0f, 0.0f, 0.0f, 0.0f, 0.0f, 9.81f, 0.2f, -0.2f, 0.2f}; /**< Measurement vector */
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static float x_aposteriori_k[12]; /**< states */
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static float P_aposteriori_k[144] = {100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 100.0f, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 100.0f, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 0, 100.0f,
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}; /**< init: diagonal matrix with big values */
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static float x_aposteriori[12];
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static float P_aposteriori[144];
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/* output euler angles */
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static float euler[3] = {0.0f, 0.0f, 0.0f};
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static float Rot_matrix[9] = {1.f, 0, 0,
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0, 1.f, 0,
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0, 0, 1.f
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}; /**< init: identity matrix */
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static bool thread_should_exit = false; /**< Deamon exit flag */
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static bool thread_running = false; /**< Deamon status flag */
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static int attitude_estimator_ekf_task; /**< Handle of deamon task / thread */
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@@ -153,7 +121,7 @@ int attitude_estimator_ekf_main(int argc, char *argv[])
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attitude_estimator_ekf_task = task_spawn("attitude_estimator_ekf",
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SCHED_DEFAULT,
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SCHED_PRIORITY_MAX - 5,
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12000,
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12400,
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attitude_estimator_ekf_thread_main,
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(argv) ? (const char **)&argv[2] : (const char **)NULL);
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exit(0);
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@@ -193,6 +161,38 @@ int attitude_estimator_ekf_main(int argc, char *argv[])
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*/
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int attitude_estimator_ekf_thread_main(int argc, char *argv[])
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{
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const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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float dt = 0.005f;
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/* state vector x has the following entries [ax,ay,az||mx,my,mz||wox,woy,woz||wx,wy,wz]' */
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float z_k[9] = {0.0f, 0.0f, 0.0f, 0.0f, 0.0f, 9.81f, 0.2f, -0.2f, 0.2f}; /**< Measurement vector */
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float x_aposteriori_k[12]; /**< states */
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float P_aposteriori_k[144] = {100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 100.f, 0, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 100.0f, 0, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 100.0f, 0,
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0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 0, 100.0f,
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}; /**< init: diagonal matrix with big values */
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float x_aposteriori[12];
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float P_aposteriori[144];
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/* output euler angles */
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float euler[3] = {0.0f, 0.0f, 0.0f};
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float Rot_matrix[9] = {1.f, 0, 0,
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0, 1.f, 0,
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0, 0, 1.f
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}; /**< init: identity matrix */
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// print text
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printf("Extended Kalman Filter Attitude Estimator initialized..\n\n");
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fflush(stdout);
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